LEMUR-2-MYRA, 66787
Orbit data source: Space-Track
LEMUR-2-MYRA, 66787 is an American payload satellite in SSO that was launched on Fri, 28 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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66787 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 4U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.045 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LEMUR-2-MYRA
1 66787U 25276EB 26238.14204291 .00002907 00000-0 23266-3 0 9990
2 66787 97.5286 306.7748 0015855 275.3204 84.6211 15.00853621 40709Epoch: 2026-08-26T03:24Z
TLE epoch observation values (Epoch: 2026-08-26T03:24:32.507Z)
Latitude
-0.00005°
Longitude
-78.75993°
Altitude
566.309 km
Speed
7.579 km/s
True Right ascension
20h 27m 05s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
19:05:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.262 km
Perigee altitude
550.257 km
Semi-major axis
6,939.396 km
Eccentricity
0.00159
Inclination
97.5286°
RAAN
306.7748°
Arg. of periapsis
275.3204°
True anomaly
84.80202°
Mean anomaly
84.6211°
Eccentric anomaly
84.71156°
Mean motion
3.75457 °/min
Orbital period
95.88 mins
BSTAR
0.00023266
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Other satellites on launch #276 in the year 2025 (2025-11-28 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.LEMUR-2-MYRA Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-27 05:08:04.840Z | 194.585° SSW | 2026-08-27 05:11:04.840Z | 260.23° W | 33.631° | 2026-08-27 05:14:04.840Z | 327.994° NNW |
| 5 mins | 2026-08-27 16:48:04.840Z | 50.342° ENE | 2026-08-27 16:50:04.840Z | 89.347° E | 23.214° | 2026-08-27 16:53:04.840Z | 146.859° SSE |
| 5 mins | 2026-08-27 18:23:04.840Z | 332.039° NNW | 2026-08-27 18:25:04.840Z | 294.263° NW | 21.426° | 2026-08-27 18:28:04.840Z | 241.447° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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